FORCETALLY
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At a glance
Fattah-2larger figure on 1 of 1
Hwasong-11Alarger figure on 0 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Mass
Single source3,415–8,729 kg (7,529–19,244 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Fattah-2 | Hwasong-11A |
|---|---|---|
| Type | Hypersonic missile[source] | Short-range ballistic missile[source] |
| Used by | Iran[source] | North Korea ( Korean People's Army Strategic Force ) Russia[source] |
| Designer | IRGC engineers[source] | — |
| Manufacturer | AIO[source] | February 11 Plant[source] |
| Warhead | Conventional Warhead[source] | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] |
| Propellant | Stage 1: Solid‑Fuel Booster Stage 2: Liquid‑Fuel HGV[source] | Solid composite[source] |
| Launch platform | Road‑mobile TEL[source] | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] |
| Country of origin | Iran[source] Iran[source] | — |
| Place of origin | — | North Korea[source] |
| In service | — | 2019–present[source] |
| Wars | — | Russo-Ukrainian war[source] |
| Designed | — | 2018[source] |
| Developed into | — | See § Variants[source] |
| Engine | — | Solid-fueled engine[source] |
| Flight altitude | — | 50–60 km (31–37 mi)[source] |
| Guidance system | — | Inertial navigation system (INS), possible satellite navigation[source] |
| Accuracy | — | 35–200 m (115–656 ft)[source] |